High-Resolution Thermal Profiling of a Combustor in a Non-Dedicated Test Using Thermal History Coatings

D. Peral, A. Zaid, Christoph Benninghoven, Silvia Araguás-Rodríguez, D. Kluß, S. Karagiannopoulos, Robert Krewinkel, J. Feist
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引用次数: 1

Abstract

The requirement for reduced emissions and the growing demand on gas turbine efficiency are in part met through increasing firing temperatures. However, development budgets leave only limited time for dedicated thermal testing. Consequently, manufacturers are seeking novel temperature measurement technologies to validate new engine designs. This paper will demonstrate how a new temperature mapping technology can be utilized for non-dedicated (multi-cycling) testing while still delivering high-resolution temperature data in a non-dedicated test on a combustor of an industrial gas turbine. Typically, thermocouples are used to monitor the temperature during tests, but they only provide one data point. Colour changing thermal paints are used to deliver measurements over complete surfaces, but they require dedicated testing with short-duration exposure, necessitating dismantling and re-assembling the engine for further testing. Thermal History Coatings (THC) present an alternative solution to providing high-density temperature information. This coating permanently changes consistent with the maximum temperature of exposure during test. A laser-based instrumentation technique is then used to obtain temperatures. The maximum temperature profile of the surface can be determined through a customized calibration. Given the complex cooling system of a combustor, the high temperatures and the long-time exposure, this case offers a unique possibility for the testing of the coating under real engine conditions. The coated region covered the external surface of the can. Highly significant is the number of measurement points in excess of 7,000 (2 × 2 mm resolution, which enables advanced analysis. This provides insight into the impact of local features, e.g. the region adjacent to a cooling hole. The temperature profile is compared to a CFD-CHT model and thermocouple measurements for the calibration of cooling pre-design methods.
在非专用测试中使用热历史涂层的燃烧器的高分辨率热剖面
减少排放的要求和对燃气轮机效率日益增长的需求部分是通过提高燃烧温度来满足的。然而,开发预算只留下有限的时间用于专门的热测试。因此,制造商正在寻求新的温度测量技术来验证新的发动机设计。本文将演示如何将一种新的温度映射技术用于非专用(多循环)测试,同时在工业燃气轮机燃烧室的非专用测试中仍然提供高分辨率温度数据。通常,热电偶用于监测测试期间的温度,但它们只提供一个数据点。变色热漆用于对整个表面进行测量,但它们需要短时间暴露的专用测试,需要拆卸和重新组装发动机以进行进一步测试。热历史涂层(THC)为提供高密度温度信息提供了另一种解决方案。在测试过程中,涂层会随着暴露的最高温度而永久变化。然后使用基于激光的仪器技术来获得温度。表面的最高温度分布可以通过定制的校准来确定。考虑到燃烧室复杂的冷却系统、高温和长时间的暴露,这种情况为在真实发动机条件下测试涂层提供了独特的可能性。涂覆区域覆盖罐的外表面。高度重要的是测量点的数量超过7,000 (2 × 2毫米分辨率),这使得高级分析成为可能。这可以深入了解局部特征的影响,例如邻近冷却孔的区域。温度分布与CFD-CHT模型和热电偶测量相比较,用于冷却预设计方法的校准。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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